2-ft 6-in.×2-ft 3-in. tunnel, for speeds ranging from Mach 1.4 to 3.5, completed at Aircraft Research Assn, Bedford; tunnel is driven by 13,750-hp axial compressor which also serves to evacuate ventilated working section of transonic tunnel. (See also Aircraft Eng v 31 n 361 Mar 1959 p 81-3; Engineer v 207 n 5375 Jan 30 1959 p 179; Aeroplane v 96 n 2473 Jan 23 1959 p 97-9)
New A.R.A. supersonic wind tunnel
Engineering
Engineering ; 187 , n 4848
1959
2 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
New A.R.A. supersonic wind tunnel
Engineering Index Backfile | 1959
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New A.R.A. supersonic wind tunnel
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The New A.R.A. Supersonic Wind Tunnel
Emerald Group Publishing | 1959
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